N705CK
Registered owner: KALITTA AIR LLC, MI (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| KALITTA AIR LLC | Operator | 2021-11-29 – 2021-11-29 | Operator named in NTSB report |
| KALITTA AIR LLC (KCSA) | Operator | 2021-11-29 – 2021-11-29 | Operator named in NTSB report |
Accident & incident history
Maintenance disclosures
DOOR F/D OVHD. OPENED AND CLOSED OVERHEAD HATCH, VERIFIED LATCHES TO BE OPERATING NORMAL IAW AMM 52-21-00. NO DEFECTS NOTED.
POSSIBLE CRACK ON R/H FUSELAGE AT APPROX STA 2360 STRINGER 17R
LWR FUSELAGE SKIN STA 1780 NEAR S-47R HAS MARKED SKIN DAMAGE.
#1 EMERGENCY DESCENT DEVICE DAMAGED/ SEAL BROKEN
L/H LBL 11.33 INTERCOSTAL LUG FITTING AT STA 1000 HAS CRACK INDICATION
LEFT LONGERON EXTENSION FITTING HAS CRACK INDICATION.
R/H LONGERON EXTENSION FITTING FOUND TO HAVE CRACKED. END OF CRACK MARKED.
NOSE CARGO DOOR STA 178 RBL 7, STR 46R HAS MARKED LIGHTNING STRIKE DAMAGE.
SMOKE CREW REST. TRANSFERRED TO DMI 100191197 IAW B747 MEL 26-14-2-1-2 CAT C DUE 4-23-25 PLACARDS INSTALLED (M) PROCEDURES COMPLIED WITH. REMOVED AND REPLACED PACK 3 WATER SEPERATOR COALESCER BAG IAW B747-400 AMM 21-51-05. OPERATIONS AND LEAK CHECK GOOD. NO DEFECTS NOTED, THIS CLEARS DMI 100191197.
ENGINE #2 SEVERE DAMAGE. PERFORMED N1 AND N2 LOCKOUT PER AMM 71-00-30 AND E50 #13891 FOR 3 ENGINE FERRY FLIGHT. ENGINE #2 SEVERE DAMAGE. REMOVED AND REPLACED #2 ENGINE IAW B747-400 AMM 71-00-00, REFERENCE TASK CARD NUMBER 71-002-00-00 ITEM 1 MET 7050420706 FOR WORK PERFORMED AND ORIGINAL SIGNATURES, NO DEFECTS NOTED.
100233439 - SMOKE CREW REST ENGINE-INDICATING AND CREW-ALERTING SYSTEM ON TAKE OFF, SELF CORRECTED. PERFORMED FIRE SYSTEM TEST. ALL PASSED AND CREW REST SMOKE DETECTORS SELF TEST ALL GOOD IAW B747 AMM 26-13-00. PERFORMED CONDITIONAL INSPECTION FOR SMOKE OR FUMES IN THE COCKPIT IAW B747 AMM 05-51-56 NO DEFECTS NOTED.
100233442 - SMOKE CREW REST ENGINE-INDICATING AND CREW-ALERTING SYSTEM ON TAKE OFF AT APPROXIMATELY 1600. WET SOCK SMELL. SELF CORRECTED. PERFORMED FIRE TEST AND CREST SMOKE DETECTORS SELF TEST. ALL PASS IAW B747 AMM 26-13-00. PERFORMED CONDITIONAL INSPECTION FOR SMOKE AND FUMES IN COCKPIT IAW B747 AMM 05-51-56. CLEARED WATER FROM PACK 3 DUCT IAW B747 AMM 21-00-01. NO FURTHER DEFECTS NOTED.
100233376 - ">SMOKE CREW REST" ENGINE-INDICATING AND CREW-ALERTING SYSTEM ON TAKEOFF. PERFORMED ADJUSTMENT/TEST CREW REST SMOKE DETECTION SYSTEM. OPERATIONAL CHECK GOOD. NO FAULTS OR MESSAGES NOTED. IN REFERENCE WITH B747-400 KA AMM 26-14-50.
100233382 - SMOKE CREW REST- ENGINE INDICATING AND CREW ALERTING SYSTEM ON TAKE OFF. PERFORMED FIRE SYSTEM TEST. ALL PASSED AND SMOKE DETECTORS OF THE CREW REST SELF TEST. ALL GOOD NO FAULTS NOTED IAW B747-400 AMM 26-13-00.
100183594 - ">SMOKE CREW REST" ENGINE-INDICATING AND CREW-ALERTING SYSTEM. PERFORMED ADJUSTMENT/TEST CREW REST SMOKE DETECTION SYSTEM IN REFERENCE WITH B747-400 KA AMM 26-14-50 OPERATIONAL CHECK GOOD NO FAULTS OR MESSAGES.
L/H WING FIXED LEADING EDGE RIB AT ILES 756 HAS DAMAGE
L/H WING FIXED LEADING EDGE RIB AT ILES 766 HAS DAMAGE
DOOR FLIGHT DECK OVERHEAD CAME ON AT LANDING. PERFORMED INSPECTION CHECK ON FLIGHT DECK OVERHEAD DOOR WITH NO DEFECTS NOTED IAW B747-400 AMM 52-21-00.
FLIGHT DECK DOOR OVERHEAD, ON LANDING, PERFORMED OPS CHECK OF FLIGHT DECK OVERHEAD ESCAPE HATCH IAW B747-400 AMM 52-23-00 OPERATIONAL CHECK GOOD.
100163728 DOOR FLIGHT DECK OVERHEAD. SECURED OVERHEAD DOOR IAW B747-400 AMM 52-21-00, OPS CHECK GOOD.
DOOR FLIGHT DECK OVERHEAD ADVISORY MESSAGE DURING CLIMB. PERFORMED OPERATIONS CHECK OF CREW OVERHEAD COMPARTMENTS DOOR VERIFIED NORMAL OPERATION IN REFERENCE WITH B747-400 AMM 52-21-00 CLEARED MESSAGE OPERATIONS CHECK GOOD.
FORWARD OVERHEAD DOOR - DOOR FLIGHT DECK OVERHEAD. CYCLED CREW OVERHEAD DOOR LATCH ASSEMBLY AND PERFORMED OPERATIONAL CHECK IN REFERENCE WITH B747-400 AMM 52-21-00 OPERATIONS CHECK GOOD, NO FURTHER ACTION REQUIRED.
AIRCRAFT COMMUNICATION ADDRESSING AND REPORTING SYSTEM RECORDED ON AND IN TIMES WHEN WE TOUCHED DOWN FORWARD OUTBOARD HANDLE ESCAPE DOOR ENGINE INDICATING AND CREW ALERTING SYSTEM MESSAGE. RESEATED ESCAPE DOOR HANDLE AS REQUIRED DOOR AND INDICATION NORMAL IAW B747-400 MAINTENANCE MANUAL 52-00-00.
CRACK FOUND AND VERIFIED BY SURFACE HFEC ON WEB AREA BY L5 DOOR STATION 2233 BETWEEN STR L21 AND L22
CORROSION FOUND AT STA 460 LBL105 UPPER CORD OF FLOOR BEAM
L-5 DOOR FWD LWR REVEAL HAS CRACK AT FASTENER HOLE
SUSPECTED CORROSION ON LOWER SURFACE OF SEAT TRACK STA 1130 @ LBL 11
SUSPECTED CORROSION ON LOWER SURFACE OF SEAT TRACK AT STA 1100 @ LBL 11
EVIDENCE OF SURFACE OF CORROSION IN MULTIPLE AREAS ON LOWER KEEL BEAM FROM APPX. STA.986 TO STA.1100
SUSPECTED CORROSION ON LOWER SURFACE OF SEAT TRACK AT STA 1190 @ LBL 11
FLAP PANEL 578IT HAS EVIDENCE OF CORROSION
CORROSION ON UPPER CAP OF FLOOR BEAM AT STA 980 LBL 65
CORROSION ON UPPER CORD OF FLOOR BEAM Â AT NUT PLATE LOCATION STA 980 & RBL 12 TO LBL 35
L-5 DOOR FWD UPPER REVEAL HAS CRACK ON EDGE
CREASE BEAM WEB HAS CRACK IN RADIUS AT STA 980 LH SIDE BETWEEN STR-4 AND STR-5
BS 1000 RBL 33 APPROX WL 190 SHEAR TIE CRACKED THROUGH ENTIRE CROSS SECTION
BS 1000 LBL 33 APPROX WL 190 SHEAR TIE CRACKED THROUGH ENTIRE CROSS SECTION
BS 2360 RBL 14 LOWER LOBE FRAME STIFFENER CRACKED 5 INCHES BELOW M.D. FLOOR
TENSION TIE R/H, BODY STA 760 IS BROKEN Â AT O/B END, FWD. SIDE.
STEEL SPLICE PLATE IS BROKEN AT Â UPPER DECK TENSION TIE, STA 760 R/H
CREASE BEAM WEB HAS CRACK IN RADIUS AT STA 980 RH SIDE BETWEEN STR-4 AND STR-5
BS 2360 LBL 32 LOWER LOBE FRAME STIFFENER CRACKED 5 INCHES BELOW M.D. FLOOR
BS 2360 LBL 14 LOWER LOBE FRAME STIFFENER CRACKED 5 INCHES BELOW M.D. FLOOR
BS 2360 RBL 32 LOWER LOBE FRAME STIFFENER CRACKED 5 INCHES BELOW M.D. FLOOR
DAMAGE TO RIGHT SIDE HORIZONTAL STAB AND RIGHT SIDE OF FUSELAGE FOUND ON LANDING INSPECTION. ADDENDUM WILL BE PROVIDED UPON MAJOR REPAIRS BEING PERFORMED AND RECTIFICATION COMPLETED.
ESCAPE REEL DOOR OPENED DURING LANDING AND REEL FELL OUT. REMOVED AND REPLACED IAW AMM 25-61-01.
STRONG ELECTRICAL SMOKE ODOR IN COCKPIT. IMMEDIATELY STOPPED WHEN FLIGHT DECK FAN WAS TURNED OFF. (S)
NR 2 PYLON INBOARD SKIRT CHAFED THROUGH RUB STRIP AT NAC STA-220. (A)
LT UPPER DECK ESCAPE DOOR AFT EMERGENCY LIGHT INOPERATIVE. (A)
EMERGENCY FLOOR LIGHT AT UPPER DECK LT DOOR INOP. (A)
NR 2 PYLON INBOARD NAC STA-220 SKIN DAMAGED. (A)
NR 3 PYLON BULKHEAD NAC STA 221.90 B-NUT HYDRAULIC PRESSURE LINE CHAFING ON BULKHEAD.
NR 1 PYLON BULKHEAD NAC STA 221.90 "B" NUT HYDRAULIC PRESSURE LINE CHAFING ON BULKHEAD.
NR 3 PYLON FRAME CRACKED AT NAC STA 268.06.
FWD PIT, AFT PALLET STOP FITTING CRACKED AT BS 962, LBL 24.
FWD PIT, SIDE RAIL SUPPORT BRACKET CRACKED AT BS 560, RBL 65.
CORROSION ON SEAT TRACK AT RBL-76 AT AT BS-1780 TO 1800.
STA 748 AT S41R TO S42R SKIN DAMAGED.
FWD PIT FLOORBEAM UPPER CHORD DAMAGED AT BS 840, RBL 53.
RIGHT WING L/E CAVITY I/B OF FS-1318 HAS CORROSION ON ANGLE AT L/E WEB DOUBLER LOWER AT ATTACH POINT.
NR 4 PYLON STA - 221 UPPER ATTACH ANGLE ON I/B SIDE IS CRACKED .5 INCH LONG.
FUSELAGE FRAME I/B FLANGE DAMAGED AT BS 1900, STR-12R.
MAIN DECK SEAT TRACK CORRODED AT BS 1895, LBL 11.
STA 2095 LBL 11 SEAT TRACK DAMAGED AT CENTER GUIDE LOCKDOWN PIN HOLE.
STA 2155 LBL 11 SEAT TRACK DAMAGED AT CENTER GUIDE LOCKDOWN PIN HOLE.
STA 2190 STR 44L TO STR 45L PILLOWING SKIN AROUND FASTENERS.
STA 1800 AT STR 37R SKIN DAMAGED.
FUSELAGE TENSION TIE SLOPING SHEAR WEB IS CRACKED IN 2 AREAS (.5 INCH) BETWEEN STA 820 TO 840, STR 10R & 10AR.
EXTERNAL FUSELAGE SKIN HAS PILLOWING SKIN AROUND FASTENERS AND 1 FASTENER WITH A POPPED HEAD AT STA 2190, STR 44L TO 45L.
FUSELAGE FRAME HAS A CRACK (.5 INCH) AT STA 434, BETWEEN STR 26L & 27L.
FUSELAGE TENSION TIE SLOPING SHEAR WEB IS CRACKED (.5 INCH) AT STA 820, BETWEEN STR 10L & 10AL.
L5 MAIN ENTRY DOOR LOWER HINGE CUTOUT WEB CORRODED AT BS 2245.31, WL 230.8.
UPPER DECK AFT LEFT EMERGENCY LIGHT INOP.
FUSELAGE SKIN DAMAGED AT BS 460 BETWEEN STR 36R AND 37R.
FUSELAGE SKIN DAMAGED AT BS 740 ABOVE STR 34L.
NR 3 PYLON STA 221.9 BULKHEAD WEB WHERE HYD LINE GOES THROUGH IS CRACKED .75 INCH.
NR 4 PYLON STA 221.9 BULKHEAD WEB WHERE HYD LINE GOES THROUGH IS CRACKED .5 INCH.
NR 3 PYLON HAS HYD PRESSURE LINE FITTING CHAFED THROUGH NAC STA 221.9 BULKHEAD WEB.
NR 3 PYLON AFT ENGINE MOUNT BULKHEAD NAC STA 221.9, WORN AT HYDRAULIC LINES.
LEFT BODY GEAR WHEEL WELL KEEL BEAM EXTERNAL STIFFENER CORRODED AT BOTTOM AT BS 1466.5, WL 97.
LT UPPER DECK ESCAPE DOOR FWD EMERGENCY LIGHT INOP.
NR 2 ENG FUEL ICING LIGHT ILL OPERATED HEATER PER AOM. LIGHT STAYED ON. VISUALLY INSPECTED ENG. FOUND FUEL LEAKING. SHUT ENGINE DOWN. REPLACED FUEL PUMP PER JT9D MM 73-11-01. MOTOR & RUN TEST GOOD PER AMM 72-00-00.
NR 1 PYLON NAC STA 221.90 BULKHEAD WORN AT HYDRAULIC PRESSURE LINE ABOVE MID SPAR.
NR 3 PYLON NAC STA 221.90 BULKHEAD WORN AT HYDRAULIC PRESSURE LINE ABOVE MID SPAR.
FOUND UPPER DECK EMERGENCY LIGHT ABOVE PASSENGER SEAT COMES ON WITH SWITCH IN THE ARMED POSITION. REMOVED AND REPLACED RIGHT EMERGENCY LIGHT IAW B747 MM 33-51-00.
LEFT BODY GEAR WHEEL WELL KEEL BEAM EXTERNAL STIFFENER CORRODED AT BOTTOM AT BS 1466.5, WL 97.
AC SMOKE IN COCKPIT WAS TERMINATED. CK LIST QRH, PG 3 ACCOMPLISHED. CONTINUED FLIGHT WITH PACK NR 1 OFF. FOUND OIL CONTAMINATION IN NR 1 ACM DUCTING. CLEANED PER AMM 21-00-01. NO OIL ODOR NOTED AFTER CLEANUP.